Flow in Serpentine Coolant Passages with Trip Strips

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Publisher : Independently Published
ISBN 13 : 9781792727153
Total Pages : 38 pages
Book Rating : 4.7/5 (271 download)

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Book Synopsis Flow in Serpentine Coolant Passages with Trip Strips by : National Aeronautics and Space Adm Nasa

Download or read book Flow in Serpentine Coolant Passages with Trip Strips written by National Aeronautics and Space Adm Nasa and published by Independently Published. This book was released on 2019 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt: Under the subject contract, an effort is being conducted at Scientific Research Associates, Inc. (SRA) to obtain flow field measurements in the coolant passage of a rotating turbine blade with ribbed walls, both in the stationary and rotating frames. The data obtained will be used for validation of computational tools and assessment of turbine blade cooling strategies. The configuration of the turbine blade passage model is given, and the measuring plane locations are given. The model has a four-pass passage with three 180 turns. This geometry was chosen to allow analyses of the velocity measurements corresponding to the heat transfer results obtained by Wagner. Two passes of the passage have a rectangular cross-section of 1.0 in x 0.5 in. Another two passes have a square cross-section of 0.5 in x 0.5 in. Trips with a streamwise pitch to trip height (P/e) = 5 and trip height to coolant passage width (e/Z) = 0.1, were machined along the leading and trailing walls. These dimensions are typical of those used in turbine blade coolant passages. The trips on these walls are staggered by the half-pitch. The trips are skewed at +/- 45 deg, and this allows the effect of trip orientation to be examined. Experiments will be conducted with flow entering the model through the 1.0 in x 0.5 in rectangular passage (Configuration C) and the 0.5 in x 0. 5 in square passage (Configuration D) to examine the effect of passage aspect ratio. Velocity measurements were obtained with a Reynolds number (Re) of 25,000, based on the hydraulic diameter of and bulk mean velocity in the half inch square passage. The coordinate system used in presenting the results for configurations C and D, respectively, is shown. The first, second and third passes of the passage will be referred to as the first, second and third passages, respectively, in later discussion. Streamwise distance (x) from the entrance is normalized by the hydraulic diameter (D). Vertical (y) and tangential (z) distances are normali...

Flow in Rotating Serpentine Coolant Passages With Skewed Trip Strips

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Publisher :
ISBN 13 :
Total Pages : 172 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Flow in Rotating Serpentine Coolant Passages With Skewed Trip Strips by :

Download or read book Flow in Rotating Serpentine Coolant Passages With Skewed Trip Strips written by and published by . This book was released on 1996 with total page 172 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Flow in Rotating Serpentine Coolant Passages with Skewed Trip Strips

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Publisher : Createspace Independent Publishing Platform
ISBN 13 : 9781723082313
Total Pages : 168 pages
Book Rating : 4.0/5 (823 download)

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Book Synopsis Flow in Rotating Serpentine Coolant Passages with Skewed Trip Strips by : National Aeronautics and Space Administration (NASA)

Download or read book Flow in Rotating Serpentine Coolant Passages with Skewed Trip Strips written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-17 with total page 168 pages. Available in PDF, EPUB and Kindle. Book excerpt: Laser velocimetry was utilized to map the velocity field in serpentine turbine blade cooling passages with skewed trip strips. The measurements were obtained at Reynolds and Rotation numbers of 25,000 and 0.24 to assess the influence of trips, passage curvature and Coriolis force on the flow field. The interaction of the secondary flows induced by skewed trips with the passage rotation produces a swirling vortex and a corner recirculation zone. With trips skewed at +45 deg, the secondary flows remain unaltered as the cross-flow proceeds from the passage to the turn. However, the flow characteristics at these locations differ when trips are skewed at -45 deg. Changes in the flow structure are expected to augment heat transfer, in agreement with the heat transfer measurements of Johnson, et al. The present results show that trips are skewed at -45 deg in the outward flow passage and trips are skewed at +45 deg in the inward flow passage maximize heat transfer. Details of the present measurements were related to the heat transfer measurements of Johnson, et al. to relate fluid flow and heat transfer measurements. Tse, David G.N. and Steuber, Gary Glenn Research Center VELOCITY DISTRIBUTION; TURBINE BLADES; FLOW DISTRIBUTION; CHANNEL FLOW; ROTATING FLUIDS; HEAT TRANSFER; COOLING; FLUID FLOW; SERPENTINE; CURVATURE; VORTICES; SWIRLING; LASER DOPPLER VELOCIMETERS; FLOW MEASUREMENT; CROSS FLOW; FLOW CHARACTERISTICS; CORIOLIS EFFECT...

1996 Coolant Flow Management Workshop

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Publisher :
ISBN 13 :
Total Pages : 356 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis 1996 Coolant Flow Management Workshop by :

Download or read book 1996 Coolant Flow Management Workshop written by and published by . This book was released on 1997 with total page 356 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Flow in a Rotating Square Serpentine Coolant Passage with Skewed Trips

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ISBN 13 :
Total Pages : 0 pages
Book Rating : 4.:/5 (137 download)

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Book Synopsis Flow in a Rotating Square Serpentine Coolant Passage with Skewed Trips by : David G. N. Tse

Download or read book Flow in a Rotating Square Serpentine Coolant Passage with Skewed Trips written by David G. N. Tse and published by . This book was released on 1997 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: Presented at the International Gas Turbine & Aeroegine Congress & Exhibition, Orlando, FL, Jun 2-Jun 5, 1997.

Scientific and Technical Aerospace Reports

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ISBN 13 :
Total Pages : 594 pages
Book Rating : 4.:/5 (319 download)

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Book Synopsis Scientific and Technical Aerospace Reports by :

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1992 with total page 594 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Effects of Rotation on Coolant Passage Heat Transfer. Volume 2: Coolant Passages with Trips Normal and Skewed to the Flow

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ISBN 13 :
Total Pages : 132 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Effects of Rotation on Coolant Passage Heat Transfer. Volume 2: Coolant Passages with Trips Normal and Skewed to the Flow by :

Download or read book Effects of Rotation on Coolant Passage Heat Transfer. Volume 2: Coolant Passages with Trips Normal and Skewed to the Flow written by and published by . This book was released on 1993 with total page 132 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Heat Transfer in Gas Turbines

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Publisher : Witpress
ISBN 13 :
Total Pages : 544 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Heat Transfer in Gas Turbines by : Bengt Sundén

Download or read book Heat Transfer in Gas Turbines written by Bengt Sundén and published by Witpress. This book was released on 2001 with total page 544 pages. Available in PDF, EPUB and Kindle. Book excerpt: This title presents and reflects current active research on various heat transfer topics and related phenomena in gas turbine systems. It begins with a general introduction to gas turbine heat transfer, before moving on to specific areas.

Paper

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Publisher :
ISBN 13 :
Total Pages : 544 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Paper by :

Download or read book Paper written by and published by . This book was released on 1998 with total page 544 pages. Available in PDF, EPUB and Kindle. Book excerpt:

ASME Technical Papers

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ISBN 13 :
Total Pages : 574 pages
Book Rating : 4.0/5 ( download)

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Download or read book ASME Technical Papers written by and published by . This book was released on 2000 with total page 574 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aeronautical Engineering

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ISBN 13 :
Total Pages : 538 pages
Book Rating : 4.3/5 (91 download)

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Download or read book Aeronautical Engineering written by and published by . This book was released on 1991 with total page 538 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Heat Transfer in Rotating Serpentine Passages with Selected Model Orientation for Smooth Or Skewed Trip Walls

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Publisher :
ISBN 13 :
Total Pages : 14 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Heat Transfer in Rotating Serpentine Passages with Selected Model Orientation for Smooth Or Skewed Trip Walls by :

Download or read book Heat Transfer in Rotating Serpentine Passages with Selected Model Orientation for Smooth Or Skewed Trip Walls written by and published by . This book was released on 1993 with total page 14 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Thermal Engineering in Power Systems

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Publisher : WIT Press
ISBN 13 : 1845640624
Total Pages : 417 pages
Book Rating : 4.8/5 (456 download)

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Book Synopsis Thermal Engineering in Power Systems by : Ryoichi Amano

Download or read book Thermal Engineering in Power Systems written by Ryoichi Amano and published by WIT Press. This book was released on 2008 with total page 417 pages. Available in PDF, EPUB and Kindle. Book excerpt: Research and development in thermal engineering for power systems are of significant importance to many scientists who are engaged in research and design work in power-related industries and laboratories. This book focuses on variety of research areas including Components of Compressor and Turbines that are used for both electric power systems and aero engines, Fuel Cells, Energy Conversion, and Energy Reuse and Recycling Systems. To be competitive in today's market, power systems need to reduce the operating costs, increase capacity factors and deal with many other tough issues. Heat Transfer and fluid flow issues are of great significance and it is likely that a state-of-the-art edited book with reference to power systems will make a contribution for design and R&D engineers and the development towards sustainable energy systems.

NASA Technical Memorandum

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ISBN 13 :
Total Pages : 492 pages
Book Rating : 4.:/5 (319 download)

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Download or read book NASA Technical Memorandum written by and published by . This book was released on 1994 with total page 492 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Monthly Catalog of United States Government Publications

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ISBN 13 :
Total Pages : 1000 pages
Book Rating : 4.:/5 (319 download)

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Download or read book Monthly Catalog of United States Government Publications written by and published by . This book was released on 1996-07 with total page 1000 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Research Strategy for Modeling the Complexities of Turbine Heat Transfer

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ISBN 13 :
Total Pages : 30 pages
Book Rating : 4.:/5 (317 download)

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Download or read book Research Strategy for Modeling the Complexities of Turbine Heat Transfer written by and published by . This book was released on 1996 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA SP.

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ISBN 13 :
Total Pages : 548 pages
Book Rating : 4.:/5 (319 download)

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Book Synopsis NASA SP. by :

Download or read book NASA SP. written by and published by . This book was released on 1992 with total page 548 pages. Available in PDF, EPUB and Kindle. Book excerpt: